journal article·2006-11

Closed form solution for strain energy release rate distribution in debonded one-edge free postbuckled composite flanged joints

Hyonny Kim

Composites Science and Technology· Volume 66· Issue 14
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Abstract

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Research context

OpenAlex topics: Mechanical Behavior of Composites · Fatigue and fracture mechanics · Composite Structure Analysis and Optimization

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References (16)

Show source-provided references
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4. Speir EE, Arnold RR, Kedward KT. Stability critical compression members. In: Herakovich CT, Tarnopol’skii YM, editors. Handbook of composites. vol. 2; 1989 [chapter 11].
5. Kim H, Kwon H, Keune JN. Buckling initiation and debond growth in adhesively bonded composite flanges, AIAA Paper No. 2003-1996. In: Proceedings of the AIAA/ASME/ASCE/AHS/ASC 44th structures, structural dynamics, and materials conference, April 7–10. Norfolk, VA; 2003.
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10. Two-dimensional modelling of compressive failure in delaminated laminates10.1177/002199838501900105 ↗
11. Efficient modeling of postbuckling delamination growth in composite laminates using plate elements10.2514/3.13038 ↗
12. A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multiaxial loading
13. Fatigue life methodology for bonded composite skin/stringer configurations10.1520/CTR10561J ↗
14. Krueger R. A Shell/3D Modeling Technique for the analysis of delaminated composite laminates. NASA Technical Memorandum, NASA/TM-2000-210287, June; 2000.
15. Hibbitt, Karlsson, and Sorensen Inc., ABAQUS Version 6.3-3; 2003.
16. Reeder JR. An evaluation of mixed mode delamination failure criteria, NASA Technical Memorandum 104210, February; 1992.